EP3201440A1 - Turbine à gaz à dispositif de levage - Google Patents

Turbine à gaz à dispositif de levage

Info

Publication number
EP3201440A1
EP3201440A1 EP15797887.5A EP15797887A EP3201440A1 EP 3201440 A1 EP3201440 A1 EP 3201440A1 EP 15797887 A EP15797887 A EP 15797887A EP 3201440 A1 EP3201440 A1 EP 3201440A1
Authority
EP
European Patent Office
Prior art keywords
gas turbine
manhole
lifting device
crane system
crane
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP15797887.5A
Other languages
German (de)
English (en)
Other versions
EP3201440B1 (fr
Inventor
Andreas Griese
Dirk MÜLLER
Katrin Tritsch
Heiko Gellenthien
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Siemens AG
Original Assignee
Siemens AG
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Siemens AG filed Critical Siemens AG
Publication of EP3201440A1 publication Critical patent/EP3201440A1/fr
Application granted granted Critical
Publication of EP3201440B1 publication Critical patent/EP3201440B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B66—HOISTING; LIFTING; HAULING
    • B66C—CRANES; LOAD-ENGAGING ELEMENTS OR DEVICES FOR CRANES, CAPSTANS, WINCHES, OR TACKLES
    • B66C23/00—Cranes comprising essentially a beam, boom, or triangular structure acting as a cantilever and mounted for translatory of swinging movements in vertical or horizontal planes or a combination of such movements, e.g. jib-cranes, derricks, tower cranes
    • B66C23/18—Cranes comprising essentially a beam, boom, or triangular structure acting as a cantilever and mounted for translatory of swinging movements in vertical or horizontal planes or a combination of such movements, e.g. jib-cranes, derricks, tower cranes specially adapted for use in particular purposes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B66—HOISTING; LIFTING; HAULING
    • B66C—CRANES; LOAD-ENGAGING ELEMENTS OR DEVICES FOR CRANES, CAPSTANS, WINCHES, OR TACKLES
    • B66C23/00—Cranes comprising essentially a beam, boom, or triangular structure acting as a cantilever and mounted for translatory of swinging movements in vertical or horizontal planes or a combination of such movements, e.g. jib-cranes, derricks, tower cranes
    • B66C23/02—Cranes comprising essentially a beam, boom, or triangular structure acting as a cantilever and mounted for translatory of swinging movements in vertical or horizontal planes or a combination of such movements, e.g. jib-cranes, derricks, tower cranes with non-adjustable and non-inclinable jibs mounted solely for slewing movements
    • B66C23/025—Cranes comprising essentially a beam, boom, or triangular structure acting as a cantilever and mounted for translatory of swinging movements in vertical or horizontal planes or a combination of such movements, e.g. jib-cranes, derricks, tower cranes with non-adjustable and non-inclinable jibs mounted solely for slewing movements with particular mounting for base of column
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B66—HOISTING; LIFTING; HAULING
    • B66C—CRANES; LOAD-ENGAGING ELEMENTS OR DEVICES FOR CRANES, CAPSTANS, WINCHES, OR TACKLES
    • B66C23/00—Cranes comprising essentially a beam, boom, or triangular structure acting as a cantilever and mounted for translatory of swinging movements in vertical or horizontal planes or a combination of such movements, e.g. jib-cranes, derricks, tower cranes
    • B66C23/02—Cranes comprising essentially a beam, boom, or triangular structure acting as a cantilever and mounted for translatory of swinging movements in vertical or horizontal planes or a combination of such movements, e.g. jib-cranes, derricks, tower cranes with non-adjustable and non-inclinable jibs mounted solely for slewing movements
    • B66C23/027—Pivot axis separated from column axis
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
    • F01D25/285—Temporary support structures, e.g. for testing, assembling, installing, repairing; Assembly methods using such structures
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/80—Repairing, retrofitting or upgrading methods

Definitions

  • the present invention relates to a crane system for a gas turbine and a lifting device which can be used in the context of such a crane system, as well as a method for producing such a crane system.
  • a gas turbine When servicing a gas turbine, it may be necessary to support or lift heavy loads. For example, when replacing a burner, it usually has to be removed as a unit from or from the gas turbine. The loads to be lifted or supported are so large that specialized lifting equipment has to be used.
  • numerous gas turbines are shaped such that the maintenance ⁇ access to certain areas of the acted upon with hot gas during operation of the gas turbine components must be made via those openings, which are normally closed by the burner. To exchange about these with
  • a suitable for maintenance on a gas turbine lifting device is known for example from EP 2 543 868 A2, which can be attached to the housing of the compressor.
  • EP 2 543 868 A2 which can be attached to the housing of the compressor.
  • manhole a specially designed maintenance access
  • lifting cranes are typically used, which can be moved about a load rail system in the ceiling area of a power plant suitable.
  • the loads to be supported or lifted by the hoisting crane are received in a suitable manner, for example, by a cable system which cooperates with the hoisting crane.
  • the applied for supporting and lifting opposing forces are suitably derived by the lifting crane about the Deckenkonstrukti ⁇ on in predetermined supporting the power plant building.
  • overhead cranes and mobile crane systems can be used, which must first be brought close to the gas turbine to be serviced, to then advantageously provide a crane boom for maintenance can.
  • the forces required for lifting or supporting the loads are in this case via the crane boom in the foundation around the gas turbine around ⁇ leads.
  • a disadvantage of these devices known from the prior art is that the lifting devices to be provided are designed to be very expensive.
  • a ceiling crane for example, it is necessary to attach a complicated load rail system in the ceiling area, which is provided with suitable supports.
  • mobile cranes is responsible for providing mobility to provide a movement unit which enables ⁇ to traverse the lifting device in a suitable service position.
  • These are usually provided with wheels or wheels movement units, which also also require a relatively large amount of space, and thus significantly limit the space that may be available for maintenance personnel.
  • a crane system comprising a gas turbine, which has a manhole on its outer housing, to which end is formed to release at its opening a maintenance access to hot gas parts, wherein the manhole has a mounting portion and further comprising a Hebevor ⁇ direction, which has a Gegenbefest Trentsabites which is connected to the mounting portion such that the lifting device to be lifted by them weight forces in the outer housing the gas turbine initiates.
  • the objects underlying the invention are achieved by a lifting device, which is in particular adapted to be used in a crane system according to the Dar ⁇ position in advance as well as below, which has a counter-fastening section which is latestbil ⁇ det, with a mounting portion of a Manhole of a gas turbine to be connected such that the Hebevor ⁇ direction can initiate by them to be lifted weight forces on the counter ⁇ attachment section in the attachment section.
  • a lifting device which is in particular adapted
  • the called manhole maintenance access is in particular designed such that egg ne person of the maintenance personnel may pass through the opening in the in ⁇ nere the gas turbine.
  • This degree of accessibility is sometimes required to be able to properly service or replace components exposed to hot gas during operation of the gas turbine.
  • the attachment portion of the manhole normally serves to secure a suitable closure element, such as a lid.
  • the encryption key ment in turn allows for the intended use of the closure of the manhole in such a way that one has to worry about the Gastur ⁇ bine in regular operation no or no significant hot gas losses in the region of the manhole.
  • the attachment portion of the manhole is designed primarily to provide a suitable dacasbe ⁇ rich for the closure element available. Typically, this is designed as a round flange.
  • the ⁇ ser can then be screwed for example by means of suitable screws to the closure member and so also suffi ⁇ accordingly have tightness to safely enclose also the hot gases during normal operation of the gas turbine.
  • these fastening sections of the manhole for a connection with a geeig ⁇ Neten counter-fastening portion of the lifting device ready determine ⁇ .
  • this attachment portion with ei ⁇ nem suitable counter-fastening portion of the lifting device connected Due to the combination of Yubefest Trentsab ⁇ section and mounting portion now be lifted by the lifting device or to be supported weight forces over the relevant sections in the outer housing of the
  • Derived gas turbine This can be dispensed with a direct support, for example, with respect to the foundation on which the gas turbine stands.
  • an overhead crane is arranged on the can Ready ⁇ position approximately in the region of the ceiling portion of the overall bäudes in which the gas turbine is located can be omitted.
  • the counter-fastening portion is preferred, as well as the attachment portion formed as a round flange. It can be screwed for example by means of suitable screws with the fastening ⁇ supply section.
  • the flange knows one Thickened area, over which the forces are passed on and at the same time the lifting device receives suffi ⁇ cient stability in the assembled state. This advantageously results in a space gain , in particular in comparison to mobile lifting devices, which have to be positioned next to the gas turbine, and on the other hand the positioning of the crane system or the lifting device is already advantageously achieved on or on the gas turbine.
  • it is not necessary to properly place an external lifter before carrying out the maintenance work in order to subsequently carry out the maintenance work with this lifter.
  • mounting of the lifting device on the gas turbine via the fastening section already ensures advantageous positioning, so that maintenance work can be carried out in all or numerous sections of the outer housing of the gas turbine.
  • the support of the loads to be lifted or to be supported advantageously takes place via the outer casing of the gas turbine and ensures an introduction of force into the funda ⁇ ment on which the gas turbine is already located.
  • the ⁇ ses foundation is typically designed for exposure to high weight forces, so do not worry ge ⁇ must also bear here is that it would come to about changes in the structure of the foundation.
  • the crane according to the invention can also be provided relatively inexpensively.
  • a lifting device in the sense of the invention is intended, on the one hand, to serve for lifting, on the other hand, for lowering loads
  • a lifting device in the sense of the invention is intended, on the one hand, to serve for lifting, on the other hand, for lowering loads
  • a lifting device in addition, or may be provided only for the horizontal translation of loads.
  • the dimensions of the lifting device are typically such that all was ⁇ tung relevant areas on the gas turbine can be achieved. In particular, this relates to the area in which the burners are arranged on the gas turbine. It should also be pointed out that although the manhole providing the service access can be provided open during numerous maintenance operations, it does not have to. In this respect, the manhole is not continuously kept free during maintenance and it is even conceivable to occupy the manhole with the lifting device, while the maintenance staff operates inside the gas turbine. Should an emergency rescue of the maintenance personnel be necessary, this may possibly be carried out via a grate lid, which is kept open for emergency rescue with a latch. On the other hand, it may also be possible to recover maintenance personnel via open burner openings in such an emergency.
  • the counter-fastening section is designed as a counter-flange, which is bolted to the fastening section designed as a flange.
  • the flange is so arranged at ⁇ that it has a horizontal or horizontal orientation normal conditions of use of the gas turbine. A deviation of a few degrees, for example up to 4 ° with respect to the horizontal, should still be considered as horizontal in the context of the present application.
  • the flange is typically referred to as a manhole flange.
  • the manhole is arranged on a vertex of the outer housing.
  • a vertex in this case relates to a point on the outer casing of the gas turbine, wel ⁇ cher in the radial circumferential direction (perpendicular to the L Lucasserstre- ckungsraum the gas turbine) represents the highest point during the intended use of the gas turbine. Due to this geometric arrangement, the lifting device can be conveniently placed over all areas of the outer casing of the gas turbine to perform maintenance there.
  • the manhole may also be provided in a region of the outer housing, which is disposed offset from the apex to up to 15 ° in the circumferential direction perpendicular to the longitudinal direction of the gas turbine. This offset relates in particular to the center of gravity of the area, or in general a point in this area, which is covered by the manhole.
  • the lifting device is designed as a pillar crane, wherein in particular the counter-fastening section is attached to one end of a column of the pillar crane.
  • the pillar crane is also height adjustable.
  • a column crane has in the region of the connection of the lifting device to the gas turbine relatively small space requirement, so that a particularly maintenance-friendly and space-saving lifting device can be provided.
  • the lifting device comprises two cantilever arms or at least two cantilever arms, which are in particular designed to be pivotable.
  • the cantilever arms are pivotable about a pivot axis perpendicular to the horizontal plane (foundation plane of the gas turbine) formed in accordance with ⁇ proper use. Due to the pivotability of the boom arms, the flexibility of the use of the lifting device can be increased.
  • suitable joints at predetermined locations of the cantilever arms vorgese ⁇ hen.
  • At least one of these extension arms is designed in several parts, wherein the individual parts are in turn pivotable relative to one another.
  • the individual parts are equipped by means of suitable pivot hinges or swivel joints, by way of which the individual parts of the extension arms are fastened to one another.
  • a cantilever arm having a plurality of pivot hinges or pivot joints, which in turn increases the flexibility of the use of the respective cantilever arm.
  • At least one of the extension arms is designed as a telescopic arm. It is also conceivable ⁇ bar that at least a part of the cantilever arm is formed telescopically. According to this embodiment, increased flexibility can be achieved when working with the crane system or the lifting device. In particular, any desired maintenance area on the outer casing of the gas turbine can be ⁇ enough, so that the determination of the lifting device on the attachment portion at the appropriate Jacobbefes ⁇ tion section of the outer casing of the gas turbine can not constitute a restriction in the maintenance, as they would otherwise.
  • dargestell th in the following figures components are claimed in any combination with each other, as far as this combination can solve the problem underlying the invention.
  • Figure 1 shows a first embodiment of the invention
  • FIG. 2 shows another embodiment of the invention
  • FIG. 3 shows the embodiment of the crane system according to the invention shown in FIG. 2, together with the embodiment of the lifting device according to the invention, in a working position differing from that in FIG.
  • FIG. 4 is a flowchart representation of a first
  • Embodiment of the method according to the invention for producing a crane system shows a first embodiment of the invention shown SEN crane system 100 having an embodiment of the lifting device 30 Inventive ⁇ proper, which is attached ⁇ introduced via a counter-fixing portion 35 having an attachment portion 25 a man hole 20 on the outer housing 11 of the gas turbine 10th
  • the outer housing 11 is adjacent to the manhole 20 or another number of non with reference numeral versehe ⁇ NEN housing openings (burner ports) are available, through which the interior of the gas turbine 10 and thus the acted upon by hot gas components can be achieved by maintenance personnel.
  • the lifting device 30 itself is designed as a pillar crane, which has a column 31 which has at one end the respective counter-fastening section 35, which is connected to the
  • Attachment portion 25 of the manhole 20 is connected.
  • the connection between the two sections 25, 35 takes place by means of a flange connection, since both the fastening section 25 as the fastening flange and the counter-fastening section 35 are designed as a counter-fastening flange. Both flanges are, for example, firmly connected to each other via suitable bolts.
  • the lifting device 30, which is designed as a pillar crane, furthermore has a jib arm 36, which is provided at the end by means of a joint which is not further provided with reference numerals.
  • Swivel hinge is connected to the column 31.
  • the cantilever arm 36 which has a double T-profile or an MSH profile in cross-section (perpendicular to the longitudinal extension direction), allows a motor 41, which is connected to an input unit 42 on the column 31 by a suitable electrical supply line 40 is to perform lifting tasks.
  • the motor 41 can be moved by means of suitable and not provided with further Be ⁇ reference numbers rollers along the cantilever arm 36, while at the same overall about a not shown load cable for lifting and supporting of loads can be used.
  • suitable handling it is possible, for example, to move the extension arm 36 to a location approximately above the burner openings shown, so that after suitable positioning of the motor along the extension arm 36, it can be positioned directly in extension beyond the designated burner opening. Due to the column construction, there is sufficient space in the area of the burner openings for the maintenance personnel or another maintenance device.
  • FIG. 2 shows a further embodiment of the erfindungsge ⁇ MAESSEN crane system with another embodiment of the lifting apparatus of the invention 30.
  • the lifting device 30 has two cantilever arms 36, 37, both of which are respectively secured via a not further Being Trapped by reference numeral pivot on a column 31st
  • the pivot joint allows a pivoting of the respective arm 36, 37 by more than 180 °, so that in turn by means of both extension arms 36, 37 all maintenance technically required areas of the outer housing 11 of the gas turbine 10 can be achieved.
  • the lifting device 30 provides two extension arms 36 and 37, which can also be used simultaneously. As a result, the flexibility in use of the present embodiment is increased.
  • a plurality of cantilever arms 36, 37 may also be provided.
  • the two extension arms 36, 37 are in turn made of several parts ⁇ , the individual parts are in turn pivotally mounted against each other.
  • joints 38 and 39 in the respective cantilever arms 36 and 37 are provided.
  • the joints 38 and 39 thus define the individual parts of the respective cantilever arm 36, 37 which are not provided with reference numerals.
  • the adjustment or pivoting of the extension arms 36, 37 can be done manually with or without aids.
  • Help ⁇ medium are about suitable guide cables, which are attached to the off ⁇ legerarmen 36, 37.
  • the parts of the extension arms 36, 37 provided with the respective motors 41 may be telescopic. It may also be sufficient that the terminal portions of the respective cantilever arms 36, 37 have a double-T-profile or a profile on ⁇ MSH in cross section, can be moved along which the respective motor 41st
  • the attachment of the lifting device 30 to the outer housing 11 of the gas turbine 10 is again effected by means of a suitable counter-fastening portion 35 which is attached to the Befest Drsab ⁇ section 25 of a manhole 20.
  • the manhole 20 is also arranged on a vertex of the outer housing 11 in the present case. This can be easily understood on the basis of the Krüm ⁇ tion of the outer housing 11 shown.
  • Figure 3 shows the embodiment of the crane system 100 according to the invention already shown in Figure 2 along with the corresponding embodiment of the lifting device of the invention 30, shown in Figure 3
  • Radioti ⁇ on differs only to the effect of the embodiment shown in Figure 2, that the individual parts of the Boom arms 36 and 37 pivoted about the joints 38 and 39 WUR ⁇ the that the one arm to 36, 37 associated parts are largely aligned parallel to each other.
  • the ⁇ ser representation can be easily seen that not only portions of the outer casing 11 of the gas turbine 10 through the cantilever arms 36, 37 can be achieved, which are spaced from the large man ⁇ hole 20 but also maintenance areas, which lie in the immediate vicinity of the manhole.
  • the present operating position may be a transport position in which the crane system 100 can be removed from or placed on the gas turbine 10, without hindering assembly work.
  • the column 31 of the lifting ⁇ device 30 is designed to be adjustable in height, so that the lifting device 30 can be adjusted as a whole in height.
  • FIG. 4 shows an embodiment of the method according to the invention for producing a crane system in a flowchartatic representation.
  • the following steps are vorgese ⁇ hen:

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Load-Engaging Elements For Cranes (AREA)
  • Jib Cranes (AREA)

Abstract

L'invention concerne un système de grue (100) comprenant une turbine à gaz (10), laquelle présente sur son enveloppe extérieure (11) un trou d'homme (20), dont l'ouverture est destinée à libérer l'accès aux pièces exposées aux gaz chaud de la turbine à gaz (10) en vue d'un entretien, le trou d'homme (20) comprenant une partie de fixation (25). Le système comprend en outre un dispositif de levage (30), lequel présente une partie de fixation complémentaire (35) qui est reliée à la partie de fixation (25) du trou d'homme (20), de telle manière que le dispositif de levage (30) introduit des forces de gravité qu'il doit soulever dans l'enveloppe extérieure (11) de la turbine à gaz (10).
EP15797887.5A 2014-11-18 2015-11-05 Turbine à gaz dotée d'un dispositif de levage Active EP3201440B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
EP14193683.1A EP3023606A1 (fr) 2014-11-18 2014-11-18 Turbine à gaz dotée d'un dispositif de levage
PCT/EP2015/075817 WO2016078926A1 (fr) 2014-11-18 2015-11-05 Turbine à gaz à dispositif de levage

Publications (2)

Publication Number Publication Date
EP3201440A1 true EP3201440A1 (fr) 2017-08-09
EP3201440B1 EP3201440B1 (fr) 2018-10-03

Family

ID=51932224

Family Applications (2)

Application Number Title Priority Date Filing Date
EP14193683.1A Withdrawn EP3023606A1 (fr) 2014-11-18 2014-11-18 Turbine à gaz dotée d'un dispositif de levage
EP15797887.5A Active EP3201440B1 (fr) 2014-11-18 2015-11-05 Turbine à gaz dotée d'un dispositif de levage

Family Applications Before (1)

Application Number Title Priority Date Filing Date
EP14193683.1A Withdrawn EP3023606A1 (fr) 2014-11-18 2014-11-18 Turbine à gaz dotée d'un dispositif de levage

Country Status (6)

Country Link
US (1) US10273121B2 (fr)
EP (2) EP3023606A1 (fr)
JP (1) JP2018503016A (fr)
KR (1) KR101818026B1 (fr)
CN (1) CN107001011A (fr)
WO (1) WO2016078926A1 (fr)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3053322B1 (fr) * 2016-06-30 2020-12-04 Manitowoc Crane Group France Installation et procede de support incluant une grue a tour pour supporter un cable electrique de ligne a haute tension
KR101862933B1 (ko) * 2016-10-13 2018-05-31 두산중공업 주식회사 가스 터빈
DE102017200367A1 (de) 2017-01-11 2018-07-12 Siemens Aktiengesellschaft Verfahren zur Montage und/oder Demontage von Komponenten einer ein Turbinengehäuse aufweisenden Turbine, Adapter und System zur Verwendung in dem Verfahren sowie Verwendung eines Adapters
KR102185605B1 (ko) 2017-07-12 2020-12-02 지멘스 악티엔게젤샤프트 가스 터빈용 장착 시스템 및 연관 가스 터빈
CN109437027B (zh) * 2018-12-19 2023-09-26 厦门厦工中铁重型机械有限公司 一种盾构机刀具吊装装置
DE102022210466A1 (de) 2022-10-04 2024-04-04 Siemens Energy Global GmbH & Co. KG Aufhängungssystem für ein Mannloch, Gasturbine und Verfahren
CN115849167A (zh) * 2023-03-01 2023-03-28 瓦兰热能设备(无锡)有限公司 一种用于更换燃烧器的吊装结构

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NZ241415A (en) * 1992-01-27 1995-04-27 Air New Zealand Ltd Gas turbine engine transporting frames
JP3577039B2 (ja) * 1999-11-17 2004-10-13 ビ−エイイ− システムズ パブリック リミテッド カンパニ− 航空機組立てツールとその製造方法
EP1668244B1 (fr) * 2003-09-26 2013-06-05 Vestas Wind Systems A/S Equipement pour le montage sur le moyeu d'une eolienne et procede d'entretien d'eolienne mettant en oeuvre un tel equipement
CN102187090A (zh) * 2008-09-30 2011-09-14 维斯塔斯风力系统集团公司 用于风力涡轮机的维护起重机
CN105508154B (zh) * 2011-02-07 2018-02-13 菱重维斯塔斯海上风力有限公司 具有直升机平台装置的风轮机及其使用方法
US8814512B2 (en) * 2011-07-05 2014-08-26 United Technologies Corporation Fan disk apparatus and method
CN202671017U (zh) * 2012-05-23 2013-01-16 本科电器有限公司 热水器内胆挂具
CN202785244U (zh) * 2012-09-06 2013-03-13 江苏祥生新能源科技有限公司 用于拆装挤出机内置管模吊具
DE102013205030B4 (de) 2013-03-21 2015-10-22 Senvion Gmbh System und Verfahren zum Transportieren und Prüfen eines zur Verwendung bei einer Offshore-Windenergieanlage bestimmten Krans
US9428369B2 (en) * 2013-09-11 2016-08-30 General Electric Company Articulated slewing jib crane and wind turbine incorporating same
US9651020B2 (en) * 2013-09-24 2017-05-16 General Electric Company Portable crane for use in wind turbines
CN203638959U (zh) * 2013-12-31 2014-06-11 齐重数控装备股份有限公司 简易工作台起吊装置

Also Published As

Publication number Publication date
JP2018503016A (ja) 2018-02-01
KR20170061164A (ko) 2017-06-02
EP3023606A1 (fr) 2016-05-25
KR101818026B1 (ko) 2018-01-12
EP3201440B1 (fr) 2018-10-03
CN107001011A (zh) 2017-08-01
US10273121B2 (en) 2019-04-30
WO2016078926A1 (fr) 2016-05-26
US20170313556A1 (en) 2017-11-02

Similar Documents

Publication Publication Date Title
EP3201440A1 (fr) Turbine à gaz à dispositif de levage
DE3034013C2 (de) Deckenschwenkarm für medizinische Räume
EP1857670A1 (fr) Méthode et dispositif pour l'érection d'une tour d'une éolienne, la tour comprenant des segments
EP2134927B1 (fr) Dispositif de fixation destiné à fixer un rotor d'une turbomachine, disposé perpendiculairement par rapport à un plan horizontal, contre le basculement, et procédé d'orientation destiné à cet effet
EP3042011B1 (fr) Procédé de montage d'équipements d'une tour
EP2742213B1 (fr) Dispositif pour faire pivoter un rotor d'une turbomachine d'une première position dans une seconde position
EP3011143B1 (fr) Dispositif de rotation pour une turbine à gaz et procédés pour faire tourner un composant
WO2012175171A1 (fr) Dispositif de manutention de charges pour le levage et procédé de montage de pales de rotor d'un aérogénérateur
WO2015090282A1 (fr) Dispositif de retenue, de levage et de blocage permettant un montage sur de hauts bâtiments du type mât
EP3047083A1 (fr) Toit de protection variable
EP3538745A1 (fr) Procédé de montage et/ou démontage de composants d'une turbine comportant un carter de turbine, adaptateur, système à utiliser dans le procédé et utilisation d'un adaptateur
BE1024814A1 (de) Eine Ankoppelungsvorrichtung zum Anbringen von Transformatoren und das Verfahren zu deren Anwendung
DE102017128143B3 (de) Wartungsplattform zur Wartung von Einbauten in einem Turm für eine Windenergieanlage und Anordnung einer Wartungsplattform
EP3101271B1 (fr) Systeme et procede de transport et de levage d'une pale de rotor d'une eolienne
DE102008023670B3 (de) Montagehilfe und Verfahren zum Aufbau der Montagehilfe
EP3622164B1 (fr) Système de support pour une turbine à gaz et turbine à gaz associée
EP0320855B1 (fr) Dispositif de démolition de cheminées, en particulier des cheminées convergentes
DE102018214996A1 (de) Verfahren und Vorrichtung zur Demontage und/oder Montage eines ringförmigen Bauteils
WO2014124798A1 (fr) Grue pourvue d'un équipement de démontage d'une flèche de la grue en hauteur
EP3444471B1 (fr) Plate-forme d'entretien ainsi que dispositif d'entretien des éléments de montage dans une tour d'une éolienne et procédé de montage d'une plate-forme d'entretien
DE102021206337B4 (de) Installationsvorrichtung für einen Antennenturm und Verfahren
EP3438450B1 (fr) Plate-forme de travaux d'entretien sur une éolienne, procédé de montage d'une telle plate-forme et éolienne
DE10164514C1 (de) Hebevorrichtung zur Erhöhung von Freileitungsmasten
WO2018158045A1 (fr) Procédé de montage et/ou de démontage, dispositif conçu pour être utilisé lors de ce procédé, adaptateur de brûleur, adaptateur de transition, système et utilisation d'un robot
DE102014220193A1 (de) Kabelüberführung

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 20170420

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME

RAP1 Party data changed (applicant data changed or rights of an application transferred)

Owner name: SIEMENS AKTIENGESELLSCHAFT

DAV Request for validation of the european patent (deleted)
DAX Request for extension of the european patent (deleted)
GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

INTG Intention to grant announced

Effective date: 20180606

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

Ref country code: AT

Ref legal event code: REF

Ref document number: 1048833

Country of ref document: AT

Kind code of ref document: T

Effective date: 20181015

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

Free format text: LANGUAGE OF EP DOCUMENT: GERMAN

Ref country code: DE

Ref legal event code: R096

Ref document number: 502015006273

Country of ref document: DE

REG Reference to a national code

Ref country code: CH

Ref legal event code: NV

Representative=s name: SIEMENS SCHWEIZ AG, CH

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20181003

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181003

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: ES

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181003

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181003

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181003

Ref country code: HR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181003

Ref country code: PL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181003

Ref country code: NO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190103

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190103

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181003

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190203

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181003

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181003

Ref country code: RS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181003

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190104

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190203

Ref country code: AL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181003

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 502015006273

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181003

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20181105

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20181130

REG Reference to a national code

Ref country code: IE

Ref legal event code: MM4A

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181003

Ref country code: MC

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181003

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181003

Ref country code: SM

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181003

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181003

26N No opposition filed

Effective date: 20190704

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181003

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20181105

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20181203

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20181130

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181003

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: HU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO

Effective date: 20151105

Ref country code: MK

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20181003

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181003

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20191105

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20191105

REG Reference to a national code

Ref country code: DE

Ref legal event code: R081

Ref document number: 502015006273

Country of ref document: DE

Owner name: SIEMENS ENERGY GLOBAL GMBH & CO. KG, DE

Free format text: FORMER OWNER: SIEMENS AKTIENGESELLSCHAFT, 80333 MUENCHEN, DE

REG Reference to a national code

Ref country code: AT

Ref legal event code: MM01

Ref document number: 1048833

Country of ref document: AT

Kind code of ref document: T

Effective date: 20201105

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: AT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20201105

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: CH

Payment date: 20220209

Year of fee payment: 7

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20221130

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20221130

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: TR

Payment date: 20231017

Year of fee payment: 9

Ref country code: IT

Payment date: 20231124

Year of fee payment: 9

Ref country code: DE

Payment date: 20231127

Year of fee payment: 9